Fluid-structure interactions of variable span wings in low Reynold flows
Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pen...
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Science Publishing CorporationPublisher of International Academic Journals
2018
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iium-661982018-10-02T06:27:03Z http://irep.iium.edu.my/66198/ Fluid-structure interactions of variable span wings in low Reynold flows Salleh, Hafiz Saharin, Sanisah Azmi, Mohammad Hanafi Khan, Sher Afghan TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pencentage) is validated with experimental result from previous study. Effect of the change of wingspan on low Reynold number/flows is investigated for the wing lift coefficient, and aerodynamics efficiency. Some contour results including pressure contour is observed. The pressure contour along wingspan from each case is figured out. Science Publishing CorporationPublisher of International Academic Journals 2018-08 Article PeerReviewed application/pdf en http://irep.iium.edu.my/66198/1/66198_Fluid-structure%20interactions%20of%20variable.pdf application/pdf en http://irep.iium.edu.my/66198/2/66198_Fluid-structure%20interactions%20of%20variable_SCOPUS.pdf Salleh, Hafiz and Saharin, Sanisah and Azmi, Mohammad Hanafi and Khan, Sher Afghan (2018) Fluid-structure interactions of variable span wings in low Reynold flows. International Journal of Engineering & Technology, 7 (3.29). pp. 381-385. ISSN 2227-524X https://www.sciencepubco.com/index.php/ijet/article/view/19198/8842 10.14419/ijet.v7i3.29.19198 |
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TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics |
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TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics Salleh, Hafiz Saharin, Sanisah Azmi, Mohammad Hanafi Khan, Sher Afghan Fluid-structure interactions of variable span wings in low Reynold flows |
description |
Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pencentage) is validated with experimental result from previous study. Effect of the change of wingspan on low Reynold number/flows is investigated for the wing lift coefficient, and aerodynamics efficiency. Some contour results including pressure contour is observed. The pressure contour along wingspan from each case is figured out. |
format |
Article |
author |
Salleh, Hafiz Saharin, Sanisah Azmi, Mohammad Hanafi Khan, Sher Afghan |
author_facet |
Salleh, Hafiz Saharin, Sanisah Azmi, Mohammad Hanafi Khan, Sher Afghan |
author_sort |
Salleh, Hafiz |
title |
Fluid-structure interactions of variable span wings in low Reynold flows |
title_short |
Fluid-structure interactions of variable span wings in low Reynold flows |
title_full |
Fluid-structure interactions of variable span wings in low Reynold flows |
title_fullStr |
Fluid-structure interactions of variable span wings in low Reynold flows |
title_full_unstemmed |
Fluid-structure interactions of variable span wings in low Reynold flows |
title_sort |
fluid-structure interactions of variable span wings in low reynold flows |
publisher |
Science Publishing CorporationPublisher of International Academic Journals |
publishDate |
2018 |
url |
http://irep.iium.edu.my/66198/ http://irep.iium.edu.my/66198/ http://irep.iium.edu.my/66198/ http://irep.iium.edu.my/66198/1/66198_Fluid-structure%20interactions%20of%20variable.pdf http://irep.iium.edu.my/66198/2/66198_Fluid-structure%20interactions%20of%20variable_SCOPUS.pdf |
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2023-09-18T21:33:57Z |
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2023-09-18T21:33:57Z |
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1777412695146889216 |